The numerical simulation and evaluation of aircraft engine axial flow turbine using numerical techniques MAHE Digital Repository

The numerical simulation and evaluation of aircraft engine axial flow turbine using numerical techniques

Bhavana, G N S and Singh, Suraj and Srinivas, G (2019) The numerical simulation and evaluation of aircraft engine axial flow turbine using numerical techniques. International Journal of Mechanical and Production, 9 (4). pp. 989-994. ISSN 2249-6890

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Abstract

This research aims to improve the efficiency of an axial flow turbine by improving the boundary conditions. In the baseline paper, Sherwood number, Nusselts number for a given flow were determined. The pressure ratio was not considered in the paper

Item Type:	Article
Uncontrolled Keywords:	Axial Flow Turbines, ANSYS Fluent, Sherwood Number, Nusselt Number, Tip Losses & Efficiency
Subjects:	Engineering > MIT Manipal > Aeronautical and Automobile
Depositing User:	MIT Library
Date Deposited:	24 Jul 2019 04:52
Last Modified:	24 Jul 2019 04:52
URI:	http://eprints.manipal.edu/id/eprint/154226

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